81_FR_36247 81 FR 36139 - Airworthiness Directives; Piper Aircraft, Inc. Airplanes

81 FR 36139 - Airworthiness Directives; Piper Aircraft, Inc. Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 81, Issue 108 (June 6, 2016)

Page Range36139-36140
FR Document2016-13226

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to certain Piper Aircraft, Inc. Model PA-31-350 airplanes. The wing locations of engine TIO-540-J2B and LTIO-540-J2B in table 1 of the Applicability, paragraph (c), section are incorrect. This document corrects that error. In all other respects, the original document remains the same; however we are publishing the entire rule in the Federal Register.

Federal Register, Volume 81 Issue 108 (Monday, June 6, 2016) 
[Federal Register Volume 81, Number 108 (Monday, June 6, 2016)]
[Rules and Regulations]
[Pages 36139-36140]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2016-13226]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0338; Directorate Identifier 2014-CE-010-AD; 
Amendment 39-18495; AD 2016-08-18]
RIN 2120-AA64


Airworthiness Directives; Piper Aircraft, Inc. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: The FAA is correcting an airworthiness directive (AD) that 
published in the Federal Register. That AD applies to certain Piper 
Aircraft, Inc. Model PA-31-350 airplanes. The wing locations of engine 
TIO-540-J2B and LTIO-540-J2B in table 1 of the Applicability, paragraph 
(c), section are incorrect. This document corrects that error. In all 
other respects, the original document remains the same; however we are 
publishing the entire rule in the Federal Register.

DATES: This final rule is effective June 6, 2016.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0338; or in person at the Docket Management Facility between 9 a.m. and 
5 p.m., Monday through Friday, except Federal holidays. The AD docket 
contains this AD, the regulatory evaluation, any comments received, and 
other information. The address for the Docket Office (phone: 800-647-
5527) is Document Management Facility, U.S. Department of 
Transportation, Docket Operations, M-30, West Building Ground Floor, 
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Gary Wechsler, Aerospace Engineer, 
FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, 
College Park, Georgia 30337; telephone: (404) 474-5575; fax: (404) 474-
5606; email: [email protected].

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2016-08-18, 
Amendment 39-18495 (81 FR 26106, May 2, 2016), currently requires 
inspecting the fuel hose assembly and the turbocharger support assembly 
for proper clearance between them, inspecting each assembly for any 
sign of damage, and making any necessary repairs or replacements for 
certain Piper Aircraft, Inc. Model PA-31-350 airplanes.
    As published, the wing locations of engine TIO-540-JJ2B and LTIO-
540-J2B in table 1 of the Applicability, paragraph (c), section are 
incorrect. This document corrects that error.
    Although no other part of the preamble or regulatory information 
has been corrected, we are publishing the entire rule in the Federal 
Register.
    The effective date of this AD remains June 6, 2016.

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2016-08-18 Piper Aircraft, Inc.: Amendment 39-18495; Docket No. FAA-
2014-0338; Directorate Identifier 2014-CE-010-AD.

(a) Effective Date

    This AD is effective June 6, 2016.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Piper Aircraft, Inc. Model PA-31-350 
airplanes, serial numbers 31-5001 through 31-5004, 31-7305005 
through 31-8452024, and 31-8253001 through 31-8553002, certificated 
in any category, that are equipped with the following engines and 
fuel pump hose assemblies:

              Table 1 to Paragraph (c) of This AD--Applicable Engines and Fuel Pump Hose Assemblies
----------------------------------------------------------------------------------------------------------------
                                         Manufacturer's hose    Manufacturer's part No.
                Engine                           name                     (P/N)              Hose description
----------------------------------------------------------------------------------------------------------------
LTIO-540-J2B (right wing)............  Hose Assembly--Fuel....  Piper 39995-034........  Inlet fuel hose to
                                                                                          engine fuel pump.
TIO-540-J2B (left wing)..............  Hose, Fuel pump to       Lycoming LW-12877-6S142  Exit fuel hose from
                                        Injector.                                         engine fuel pump.
LTIO-540-J2BD (right wing)...........  Hose, Fuel pump to       Lycoming LW-12877-6S142  Exit fuel hose from
                                        Injector.                                         engine fuel pump.
TIO-540-J2BD (left wing).............  Hose Assembly--Fuel....  Piper 39995-034........  Inlet fuel hose to
                                                                                          engine fuel pump.
----------------------------------------------------------------------------------------------------------------

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code 73: Engine Fuel and Control.

(e) Unsafe Condition

    This AD was prompted by a report of an engine fire caused by a 
leak in the fuel pump inlet hose. We are issuing this AD to correct 
the unsafe condition on these products.

(f) Compliance

    Comply with this AD within the compliance times specified in 
paragraphs (g)(1) through (j)(2) of this AD, unless already done.

(g) Ensure Proper Clearance Between the Fuel Hose Assembly and the 
Turbocharger Support Assembly

    (1) Within the next 60 hours time-in-service (TIS) after June 6, 
2016 (the effective date of this AD) or within the next 6 months 
after June 6, 2016 (the effective date of this AD), whichever occurs 
first, inspect to determine the clearance between the inlet and exit 
fuel hose assemblies listed in table 1 to paragraph (c) of this AD, 
and each turbocharger support assembly, Lycoming P/N LW-18302. There 
should be a minimum 3/16-inch clearance. Do the inspection following 
the INSTRUCTIONS section of Piper Aircraft, Inc. Service Bulletin 
No. 1257A, dated August 4, 2015.
    (2) Before further flight after the inspection required in 
paragraph (g)(1) of this AD, if the measured clearance is less than 
3/16-inch, make all necessary adjustments to make the clearance a 
minimum of 3/16-inch between the inlet and exit fuel hose assemblies 
listed in table 1 to paragraph (c) of this AD and each turbocharger 
support assembly,

[[Page 36140]]

Lycoming P/N LW-18302, following the INSTRUCTIONS section of Piper 
Aircraft, Inc. Service Bulletin No. 1257A, dated August 4, 2015.

(h) Visually Inspect the Fuel Hose Assembly and Replace If Necessary

    (1) Within the next 60 hours TIS after June 6, 2016 (the 
effective date of this AD) or within the next 6 months after June 6, 
2016 (the effective date of this AD), whichever occurs first, 
visually inspect the inlet and exit fuel hose assemblies listed in 
table 1 to paragraph (c) of this AD for evidence of leaking, 
cracking, chafing, and any other sign of damage. Do the inspection 
following the INSTRUCTIONS section of Piper Aircraft, Inc. Service 
Bulletin No. 1257A, dated August 4, 2015.
    (2) Before further flight after the inspection required in 
paragraph (h)(1) of this AD, if any evidence of leaking, cracking, 
chafing, or any other sign of damage is found in any inlet or exit 
fuel host assembly listed in table 1 to paragraph (c) of this AD, 
replace the fuel hose assembly with a serviceable part. Do the 
replacement following the INSTRUCTIONS section of Piper Aircraft, 
Inc. Service Bulletin No. 1257A, dated August 4, 2015.

(i) Visually Inspect the Turbocharger Support Assembly and Replace If 
Necessary

    (1) Within the next 60 hours TIS after June 6, 2016 (the 
effective date of this AD) or within the next 6 months after June 6, 
2016 (the effective date of this AD), whichever occurs first, 
visually inspect each turbocharger support assembly, Lycoming P/N 
LW-18302, for evidence of chafing and any other signs of damage. Do 
the inspection following the INSTRUCTIONS section of Piper Aircraft, 
Inc. Service Bulletin No. 1257A, dated August 4, 2015.
    (2) Before further flight after the inspection required in 
paragraph (i)(1) of this AD, if any evidence of chafing or any other 
sign of damage is found on any turbocharger support assembly, 
replace Lycoming P/N LW-18302 with a serviceable part. Do the 
replacement following the INSTRUCTIONS section of Piper Aircraft, 
Inc. Service Bulletin No. 1257A, dated August 4, 2015.

(j) Engine Run-Up

    (1) If any fuel line component was adjusted or replaced during 
any actions required in paragraphs (g)(1) through (i)(2) of this AD, 
before further flight, perform an engine run-up on the ground to 
check for leaks. Do the engine run-up following the INSTRUCTIONS 
section of Piper Aircraft, Inc. Service Bulletin No. 1257A, dated 
August 4, 2015.
    (2) If any leaks found during the engine run-up required in 
paragraph (j)(1) of this AD emanate from any fuel line component 
adjusted, repaired, or replaced during any actions required in 
paragraphs (g)(1) through (i)(2) of this AD, before further flight, 
take all necessary corrective actions following the INSTRUCTIONS 
section of Piper Aircraft, Inc. Service Bulletin No. 1257A, dated 
August 4, 2015.

(k) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Atlanta Aircraft Certification Office (ACO), 
FAA, has the authority to approve AMOCs for this AD, if requested 
using the procedures found in 14 CFR 39.19. In accordance with 14 
CFR 39.19, send your request to your principal inspector or local 
Flight Standards District Office, as appropriate. If sending 
information directly to the manager of the ACO, send it to the 
attention of the person identified in the Related Information 
section of this AD.
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.

(l) Related Information

    For more information about this AD, contact Gary Wechsler, 
Aerospace Engineer, FAA, Atlanta ACO, 1701 Columbia Avenue, College 
Park, Georgia 30337; telephone: (404) 474-5575; fax: (404) 474-5606; 
email: [email protected].

(m) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (i) Piper Aircraft, Inc. Service Bulletin No. 1257A, dated 
August 4, 2015.
    (ii) Reserved.
    (3) For Piper Aircraft, Inc. service information identified in 
this AD, contact Piper Aircraft, Inc., 926 Piper Drive, Vero Beach, 
Florida 32960; telephone: (772) 567-4361; fax: (772) 978-6573; 
Internet: www.piper.com/home/pages/Publications.cfm.
    (4) You may view this service information at FAA, Small Airplane 
Directorate, 901 Locust, Kansas City, Missouri 64106. For 
information on the availability of this material at the FAA, call 
(816) 329-4148.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Kansas City, Missouri, on May 31, 2016.
Pat Mullen,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2016-13226 Filed 6-3-16; 8:45 am]
 BILLING CODE 4910-13-P

Federal Register / Vol. 81, No. 108 / Monday, June 6, 2016 / Rules and Regulations 36139 Ring, Bolt, Mixing Lever Gear Unit (flight DATES: This final rule is effective June As published, the wing locations of controls). 6, 2016. engine TIO–540–JJ2B and LTIO–540– Issued in Fort Worth, Texas, on May 23, J2B in table 1 of the Applicability, ADDRESSES: You may examine the AD 2016. paragraph (c), section are incorrect. This docket on the Internet at http:// Scott A. Horn, document corrects that error. www.regulations.gov by searching for Acting Manager, Rotorcraft Directorate, Although no other part of the and locating Docket No. FAA–2014– Aircraft Certification Service. preamble or regulatory information has 0338; or in person at the Docket been corrected, we are publishing the [FR Doc. 2016–13103 Filed 6–3–16; 8:45 am] Management Facility between 9 a.m. entire rule in the Federal Register. BILLING CODE 4910–13–P and 5 p.m., Monday through Friday, The effective date of this AD remains except Federal holidays. The AD docket June 6, 2016. contains this AD, the regulatory DEPARTMENT OF TRANSPORTATION evaluation, any comments received, and PART 39—AIRWORTHINESS Federal Aviation Administration other information. The address for the DIRECTIVES Docket Office (phone: 800–647–5527) is 14 CFR Part 39 Document Management Facility, U.S. ■ 1. The authority citation for part 39 Department of Transportation, Docket continues to read as follows: [Docket No. FAA–2014–0338; Directorate Operations, M–30, West Building Identifier 2014–CE–010–AD; Amendment Authority: 49 U.S.C. 106(g), 40113, 44701. Ground Floor, Room W12–140, 1200 39–18495; AD 2016–08–18] § 39.13 [Amended] New Jersey Avenue SE., Washington, RIN 2120–AA64 DC 20590. ■ 2. The FAA amends § 39.13 by adding FOR FURTHER INFORMATION CONTACT: Gary the following new airworthiness Airworthiness Directives; Piper directive (AD): Aircraft, Inc. Airplanes Wechsler, Aerospace Engineer, FAA, Atlanta Aircraft Certification Office, 2016–08–18 Piper Aircraft, Inc.: AGENCY: Federal Aviation 1701 Columbia Avenue, College Park, Amendment 39–18495; Docket No. Administration (FAA), DOT. Georgia 30337; telephone: (404) 474– FAA–2014–0338; Directorate Identifier ACTION: Final rule; correction. 2014–CE–010–AD. 5575; fax: (404) 474–5606; email: gary.wechsler@faa.gov. (a) Effective Date SUMMARY: The FAA is correcting an This AD is effective June 6, 2016. airworthiness directive (AD) that SUPPLEMENTARY INFORMATION: published in the Federal Register. That Airworthiness Directive 2016–08–18, (b) Affected ADs AD applies to certain Piper Aircraft, Inc. Amendment 39–18495 (81 FR 26106, None. Model PA–31–350 airplanes. The wing May 2, 2016), currently requires (c) Applicability locations of engine TIO–540–J2B and inspecting the fuel hose assembly and LTIO–540–J2B in table 1 of the the turbocharger support assembly for This AD applies to Piper Aircraft, Inc. Applicability, paragraph (c), section are proper clearance between them, Model PA–31–350 airplanes, serial numbers 31–5001 through 31–5004, 31–7305005 incorrect. This document corrects that inspecting each assembly for any sign of through 31–8452024, and 31–8253001 error. In all other respects, the original damage, and making any necessary through 31–8553002, certificated in any document remains the same; however repairs or replacements for certain Piper category, that are equipped with the we are publishing the entire rule in the Aircraft, Inc. Model PA–31–350 following engines and fuel pump hose Federal Register. airplanes. assemblies: TABLE 1 TO PARAGRAPH (c) OF THIS AD—APPLICABLE ENGINES AND FUEL PUMP HOSE ASSEMBLIES Manufacturer’s part No. Engine Manufacturer’s hose name Hose description (P/N) LTIO–540–J2B (right wing) ............ Hose Assembly—Fuel .................. Piper 39995–034 .......................... Inlet fuel hose to engine fuel pump. TIO–540–J2B (left wing) ................ Hose, Fuel pump to Injector ......... Lycoming LW–12877–6S142 ....... Exit fuel hose from engine fuel pump. LTIO–540–J2BD (right wing) ......... Hose, Fuel pump to Injector ......... Lycoming LW–12877–6S142 ....... Exit fuel hose from engine fuel pump. TIO–540–J2BD (left wing) ............. Hose Assembly—Fuel .................. Piper 39995–034 .......................... Inlet fuel hose to engine fuel pump. (d) Subject (g)(1) through (j)(2) of this AD, unless already turbocharger support assembly, Lycoming Joint Aircraft System Component (JASC)/ done. P/N LW–18302. There should be a minimum Air Transport Association (ATA) of America 3/16-inch clearance. Do the inspection (g) Ensure Proper Clearance Between the following the INSTRUCTIONS section of Code 73: Engine Fuel and Control. Fuel Hose Assembly and the Turbocharger Piper Aircraft, Inc. Service Bulletin No. (e) Unsafe Condition Support Assembly 1257A, dated August 4, 2015. mstockstill on DSK3G9T082PROD with RULES This AD was prompted by a report of an (1) Within the next 60 hours time-in- (2) Before further flight after the inspection engine fire caused by a leak in the fuel pump service (TIS) after June 6, 2016 (the effective required in paragraph (g)(1) of this AD, if the inlet hose. We are issuing this AD to correct date of this AD) or within the next 6 months measured clearance is less than 3/16-inch, the unsafe condition on these products. after June 6, 2016 (the effective date of this make all necessary adjustments to make the AD), whichever occurs first, inspect to clearance a minimum of 3/16-inch between (f) Compliance determine the clearance between the inlet the inlet and exit fuel hose assemblies listed Comply with this AD within the and exit fuel hose assemblies listed in table in table 1 to paragraph (c) of this AD and compliance times specified in paragraphs 1 to paragraph (c) of this AD, and each each turbocharger support assembly, VerDate Sep<11>2014 16:21 Jun 03, 2016 Jkt 238001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\06JNR1.SGM 06JNR1

36140 Federal Register / Vol. 81, No. 108 / Monday, June 6, 2016 / Rules and Regulations Lycoming P/N LW–18302, following the authority to approve AMOCs for this AD, if DEPARTMENT OF TRANSPORTATION INSTRUCTIONS section of Piper Aircraft, requested using the procedures found in 14 Inc. Service Bulletin No. 1257A, dated CFR 39.19. In accordance with 14 CFR 39.19, Federal Aviation Administration August 4, 2015. send your request to your principal inspector (h) Visually Inspect the Fuel Hose Assembly or local Flight Standards District Office, as 14 CFR Part 71 and Replace If Necessary appropriate. If sending information directly [Docket No. FAA–2016–0449; Airspace (1) Within the next 60 hours TIS after June to the manager of the ACO, send it to the Docket No. 16–ASW–2] 6, 2016 (the effective date of this AD) or attention of the person identified in the within the next 6 months after June 6, 2016 Related Information section of this AD. Amendment of Class E Airspace; (the effective date of this AD), whichever (2) Before using any approved AMOC, Clovis, NM occurs first, visually inspect the inlet and notify your appropriate principal inspector, exit fuel hose assemblies listed in table 1 to or lacking a principal inspector, the manager AGENCY: Federal Aviation paragraph (c) of this AD for evidence of of the local flight standards district office/ Administration (FAA), DOT. leaking, cracking, chafing, and any other sign certificate holding district office. ACTION: Final rule. of damage. Do the inspection following the INSTRUCTIONS section of Piper Aircraft, (l) Related Information SUMMARY: This action modifies Class E Inc. Service Bulletin No. 1257A, dated For more information about this AD, airspace extending upward from 700 August 4, 2015. (2) Before further flight after the inspection contact Gary Wechsler, Aerospace Engineer, feet above the surface at Portales required in paragraph (h)(1) of this AD, if any FAA, Atlanta ACO, 1701 Columbia Avenue, Municipal Airport, Clovis, NM. evidence of leaking, cracking, chafing, or any College Park, Georgia 30337; telephone: (404) Decommissioning of the Portales non- other sign of damage is found in any inlet or 474–5575; fax: (404) 474–5606; email: directional radio beacon (NDB), exit fuel host assembly listed in table 1 to gary.wechsler@faa.gov. cancellation of NDB approaches at paragraph (c) of this AD, replace the fuel Portales Municipal Airport, and hose assembly with a serviceable part. Do the (m) Material Incorporated by Reference implementation of area navigation replacement following the INSTRUCTIONS (1) The Director of the Federal Register section of Piper Aircraft, Inc. Service Bulletin (RNAV) procedures have made this approved the incorporation by reference No. 1257A, dated August 4, 2015. action necessary for the safety and (IBR) of the service information listed in this management of Instrument Flight Rules (i) Visually Inspect the Turbocharger paragraph under 5 U.S.C. 552(a) and 1 CFR (IFR) operations at the airport. This Support Assembly and Replace If Necessary part 51. action also updates the geographic (1) Within the next 60 hours TIS after June (2) You must use this service information as applicable to do the actions required by coordinates for Portales Municipal 6, 2016 (the effective date of this AD) or Airport to coincide with the FAA’s within the next 6 months after June 6, 2016 this AD, unless the AD specifies otherwise. (the effective date of this AD), whichever (i) Piper Aircraft, Inc. Service Bulletin No. aeronautical database. occurs first, visually inspect each 1257A, dated August 4, 2015. DATES: Effective 0901 UTC, September turbocharger support assembly, Lycoming (ii) Reserved. 15, 2016. The Director of the Federal P/N LW–18302, for evidence of chafing and (3) For Piper Aircraft, Inc. service Register approves this incorporation by any other signs of damage. Do the inspection information identified in this AD, contact reference action under Title 1, Code of following the INSTRUCTIONS section of Federal Regulations, part 51, subject to Piper Aircraft, Inc., 926 Piper Drive, Vero Piper Aircraft, Inc. Service Bulletin No. 1257A, dated August 4, 2015. Beach, Florida 32960; telephone: (772) 567– the annual revision of FAA Order (2) Before further flight after the inspection 4361; fax: (772) 978–6573; Internet: 7400.9 and publication of conforming required in paragraph (i)(1) of this AD, if any www.piper.com/home/pages/ amendments. evidence of chafing or any other sign of Publications.cfm. ADDRESSES: FAA Order 7400.9Z, damage is found on any turbocharger support (4) You may view this service information Airspace Designations and Reporting assembly, replace Lycoming P/N LW–18302 at FAA, Small Airplane Directorate, 901 with a serviceable part. Do the replacement Points, and subsequent amendments can Locust, Kansas City, Missouri 64106. For following the INSTRUCTIONS section of be viewed online at http://www.faa.gov/ information on the availability of this Piper Aircraft, Inc. Service Bulletin No. air_traffic/publications/. For further material at the FAA, call (816) 329–4148. 1257A, dated August 4, 2015. information, you can contact the (5) You may view this service information Airspace Policy Group, Federal Aviation (j) Engine Run-Up that is incorporated by reference at the Administration, 800 Independence (1) If any fuel line component was adjusted National Archives and Records Avenue SW., Washington, DC 20591; or replaced during any actions required in Administration (NARA). For information on paragraphs (g)(1) through (i)(2) of this AD, telephone: 202–267–8783. The Order is the availability of this material at NARA, call before further flight, perform an engine run- 202–741–6030, or go to: http:// also available for inspection at the up on the ground to check for leaks. Do the www.archives.gov/federal-register/cfr/ibr- National Archives and Records engine run-up following the INSTRUCTIONS locations.html. Administration (NARA). For section of Piper Aircraft, Inc. Service Bulletin information on the availability of FAA No. 1257A, dated August 4, 2015. Issued in Kansas City, Missouri, on May Order 7400.9Z at NARA, call 202–741– (2) If any leaks found during the engine 31, 2016. 6030, or go to http://www.archives.gov/ run-up required in paragraph (j)(1) of this AD Pat Mullen, federal_register/code_of_federal- emanate from any fuel line component adjusted, repaired, or replaced during any Acting Manager, Small Airplane Directorate, regulations/ibr_locations.html. actions required in paragraphs (g)(1) through Aircraft Certification Service. FAA Order 7400.9, Airspace (i)(2) of this AD, before further flight, take all [FR Doc. 2016–13226 Filed 6–3–16; 8:45 am] Designations and Reporting Points, is necessary corrective actions following the BILLING CODE 4910–13–P published yearly and effective on mstockstill on DSK3G9T082PROD with RULES INSTRUCTIONS section of Piper Aircraft, September 15. Inc. Service Bulletin No. 1257A, dated FOR FURTHER INFORMATION CONTACT: August 4, 2015. Jeffrey Claypool, Federal Aviation (k) Alternative Methods of Compliance Administration, Operations Support (AMOCs) Group, Central Service Center, 10101 (1) The Manager, Atlanta Aircraft Hillwood Parkway, Fort Worth, TX Certification Office (ACO), FAA, has the 76177; telephone (817) 222–5711. VerDate Sep<11>2014 16:21 Jun 03, 2016 Jkt 238001 PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 E:\FR\FM\06JNR1.SGM 06JNR1


Document Created: 2016-06-04 00:16:40
Document Modified: 2016-06-04 00:16:40
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionRules and Regulations
ActionFinal rule; correction.
DatesThis final rule is effective June 6, 2016.
ContactGary Wechsler, Aerospace Engineer, FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College Park, Georgia 30337; telephone: (404) 474-5575; fax: (404) 474- 5606; email: [email protected]
FR Citation81 FR 36139 
RIN Number2120-AA64
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